N935AX

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 46,044 hrs · 50,474 cycles

RIGHT OIL STRAINER CLOGGING LIGHT ILLUMINATED ON CLIMBOUT AT REDUCED THRUST. AT IDLE, THE LIGHT STAYED ILLUMINATED. SHUT DOWN RIGHT ENGINE. RIGHT ENGINE WINDMILLED FOR LESS THAN 30 MINUTES. OIL PRESSURE OBSERVED AT ZERO. REPLACED NR 2 ENGINE IAW ABX JOB CARD 9090010.

Part: FLOORBEAM — CRACKED (BS 680) · airframe 45,431 hrs · 49,862 cycles

FLOORBEAM SPLICE FITTING CRACKED AT FS 680, LEFT BUTT LINE 23. REMOVED AND REPLACED FLOORBEAM SPLICE IAW DC9 SRM 51-30-5.

Part: PAN — CRACKED (FWD CARGO DOOR) · airframe 45,431 hrs · 49,862 cycles

CRACK IN OUTER PAN OF FORWARD LOWER CARGO DOOR, AFT END OF BEAM NR 1. REMOVED AND REPLACED FORWARD LOWER CARGO DOOR IAW DC9 SRM 52-03.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 44,263 hrs · 48,676 cycles

CABIN FLOOR SUPPORT BRACE FITTING CRACKED FS 775, LONGERON 23 RIGHT. REMOVED AND REPLACED SUPPORT STRUT IAW DC-9 SRM 51-30-5 AND 51-30-2.

Part: ANGLE — CRACKED (LT PYLON) · airframe 44,263 hrs · 48,676 cycles

CRACK INDICATION ON ANGLE, UPPER INTERIOR SURFACE OF PYLON, 3RD FROM FRONT SPAR. REMOVED ANGLE, FABRICATED NEW ANGLE, REINSTALLED ANGLE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 44,263 hrs · 48,676 cycles

WEB WAS CRACKED BETWEEN LEFT UPPER RADOME GUIDE PIN AND RIVET. REPAIRED CRACKED WEB IAW DC-9 SRM 53-01.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 44,080 hrs · 48,510 cycles

CRACKED AT SHEAR PIN RECEPTICLE ON P-DOME, 11:00 POSITION. REPAIRED IAW REA D953-50852MR AND SRD 5934886-510.

Part: RIB — CRACKED (P-DOME DOOR) · airframe 44,010 hrs · 48,448 cycles

P-DOME PLUG DOOR NR 9 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05.

Part: RIB — CRACKED (PRESS BULKHEAD) · airframe 44,010 hrs · 48,448 cycles

PRESSURE DOME PLUG DOOR NR 4 STOP SUPPORT RIB CRACKED. REPAIRED AREA IAW DC-9 SRM 52-02.

Part: SKIN — DENTED (FUSELAGE) · airframe 43,935 hrs · 48,385 cycles

DENT IN FUSELAGE SKIN AT STA 837, LONGERON 22 RIGHT, 11 INCHES LONG X .75 INCH WIDTH X .020 INCH DEEP. INSTALLED PERMANENT REPAIR IAW COI 47242-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,223 hrs · 47,735 cycles

SEAT TRACK RIGHT BUTT LINE 34 LOWER INBOARD LEG WAS CORRODED. REPLACED SECTION OF TRACK STA 917 - 931 LEFT BUTT LINE 34 IAW DC-9 SRM 51-30-1.

Part: SKIN — CORRODED (T/E FLAP) · corrosion level 2 · airframe 43,223 hrs · 47,735 cycles

LEVEL II CORROSION, BULGING SKIN, CUPPED AND BROKEN FASTENERS FLAP LOWER SURFACE AT NR 3 EXPANSION JOINT. REPLACED LOWER SKIN ON RIGHT LOWER NR 3 FLAP SEGMENT IAW DC-9 SRM 51-30-2.

Part: PAN — CORRODED (FUSELAGE) · airframe 43,223 hrs · 47,735 cycles

AREA BETWEEN AFT LOWER CARGO JAMB PAN AND FUSELAGE SKIN EXFOLIATED. LEVEL I BETWEEN FS 904 AND 917. SPLICED IN NEW SECTION OF PAN IAW DC-9 SRM 53-05.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 43,223 hrs · 47,735 cycles

FLOORBEAM TO KEEL ATTACH FITTING CRACKED AFT SIDE AT FS 718. REPLACED FITTING IAW REA D953-47908.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,161 hrs · 46,750 cycles

CUSP WEB CRACKED BETWEEN STATION 870 AND 889 AT LEFT BUTT LINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.

Part: FORMER — CRACKED (FWD. CARGO) · airframe 42,161 hrs · 46,750 cycles

FORWARD LOWER CARGO DOOR FRAME CRACKED INSIDE FORWARD LOWER LIGHTENING HOLE. REPLACED ANGLE IAW DC-9 SRM.

Part: PAN — CRACKED (FWD. CARGO) · airframe 42,161 hrs · 46,750 cycles

FORWARD LOWER CARGO DOOR STOP FITTING CRACKED ON AFT EDGE OF DOOR, 2ND FROM TOP. REPAIRED AREA IAW DC-9 SRM 52-05 AND SHOP TRAVELER # ST-0148-04. NOTE: CRACK WAS IN DOOR INNER PAN, NOT THE FITTING.

Part: SUPPORT — CRACKED (FWD CARGO) · airframe 42,161 hrs · 46,750 cycles

VERTICAL FLOOR SUPPORT FITTING CRACKED F.S. 541 AT LONGERON 24 RIGHT. REPAIRED FITTING IAW DC-9 SSRM DWG K05159, DC-9 SRM 51-30-2 AND 51-30-5.

Part: SPAR — CRACKED (CENTER WING) · airframe 42,161 hrs · 46,750 cycles

LEFT UPPER REAR SPAR HAD A HORIZONTAL CRACK IN THE UPPER INBOARD CORNER FROM LEFT BUTT LINE 5 TO BUTT LINE 0. REPAIRED AREA IAW DC-9 SRM 57.

Part: SUPPORT — CRACKED (FWD CARGO) · airframe 42,161 hrs · 46,750 cycles

VERTICAL SUPPORT FITTING AT STATION 256, LONGERON 24 LEFT CRACKED. REPAIRED FITTING IAW DC-9 SSRM.

Part: SUPPORT — CRACKED (FWD CARGO) · airframe 42,161 hrs · 46,750 cycles

VERTICAL SUPPORT FITTING AT STATION 332, LONGERON 24 RIGHT CRACKED. REPAIRED AREA IAW DC-9 SSRM DWG K05159.

Part: TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 42,161 hrs · 46,750 cycles

FIRST OFFICER'S FORWARD LEFT SEAT TRACK CORRODED AT FORWARD AND AFT MOUNT AREAS. REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1.

Part: SUPPORT — CRACKED (FWD CARGO) · airframe 42,161 hrs · 46,750 cycles

VERTICAL SUPPORT FITTING AT STATION 237, LONGERON 24 RIGHT WAS CRACKED. REPLACED FITTING IAW DC-9 SSRM DWG K05159.

Part: ANGLE — CRACKED (WHEEL WELL) · airframe 42,161 hrs · 46,750 cycles

SMALL ANGLE CRACKED BENEATH KEEL, LOCATED RIGHT OF ANTI-COLLISION LIGHT WIRE FEED THROUGH. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: PANEL — CRACKED (FWD. CARGO) · airframe 42,161 hrs · 46,750 cycles

FORWARD LOWER CARGO DOOR FORWARD EDGE AT 2ND STOP FROM BOTTOM CRACKED AT STOP FITTING. REPAIRED AREA IAW DC-9 SRM 52-05 AND SHP TRAVELER # ST-0148-04.

Part: SUPPORT — CRACKED (FWD CARGO) · airframe 42,161 hrs · 46,750 cycles

VERTICAL SUPPORT FITTING AT STATION 256, LONGERON 24 RIGHT WAS CRACKED. REPLACED FITTING IAW DC-9 SSRM DWG K05159.

Part: RIB — CORRODED (LEFT WING) · airframe 42,161 hrs · 46,750 cycles

EXFOLIATION CORROSION ON LEFT WING REAR SPAR RIB, ABOVE THE CENTER ATTACH POINT OF THE INBOARD BUTE DOOR. REPLACED RIB IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-8.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 42,161 hrs · 46,750 cycles

CRACK AT RIVET ON FORWARD FACE OF STATION 37 BULKHEAD, APPROXIMATELY 18 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.

Part: BATTERY — OVERHEATED (E/E BAY) · airframe 41,942 hrs · 46,570 cycles

AIRCRAFT BATTERIES WERE OVERHEATED. REPLACED MAIN AIRCRAFT BATTERIES, BATTERY CHARGER, AND BATTERY TEMP. SENSOR. NOTE: CREW REPORTED SMOKE FROM THE E & E COMPARTMENT. CALLED CFR AND EVACUATED THE AIRCRAFT.

Part: JACKSCREW — CORRODED (HORIZ STAB) · airframe 41,741 hrs · 46,347 cycles

THE HORIZONTAL STABILIZER JACKSCREW WAS FOUND TO HAVE PITTING CORROSION ON THE UPPER THREE THREADS. THE 26TH THREAD FROM THE BOTTOM OF THE JACKSCREW WAS ALSO NOTED TO BE CHIPPED. MAINTENANCE REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM 27-40-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,248 hrs · 45,846 cycles

EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY.

Part: INTERCOSTAL — CORRODED (BS 503 -522) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT BL 0.0 BETWEEN STATION 503 AND 522. REPAIRED IAW DC9 SRM 51-30-02.

Part: INTERCOSTAL — CORRODED (BS 484 - 503) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND INTERCOSTAL CORRODED IN FORWARD LOWER CARGO COMPARTMENT BETWEEN STATION 484 AND 503 AT BL 0.0. REPLACED INTERCOSTAL IAW DC9 MM 51-30-02.

Part: FLOORBEAM — CORRODED (BS 1003) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND FLOOR SUPPORT CORRODED AT STATION 1002 AND RBL 30. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-2.

Part: SKIN — DELAMINATED (SPOILER) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND LEFT OUTBOARD SPOILER BOARD DELAMINATED INTERNALLY. REPLACED PANEL IAW DC9 MM 27-61-01.

Part: HINGE — CRACKED (TE FLAP) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-02.

Part: PANEL — CORRODED (BS 718) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND THE OVER WHEEL WELL PRESSURE PANEL CORRODED AT STATION 718 AND BL 0.0. REPLACED PRESSURE PANEL IAW DC9 SRM 51-30-2 AND ABX REA D953-35901MR.

Part: FITTING — CRACKED (BS 680) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING CRACKED AT STATION 680 AT LBL 44. REPLACED VERTICAL SUPPORT FITTING IAW DC9 SRM 51-30-02.

Part: FLOORBEAM — CRACKED (BS 680) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING CRACKED AT STATION 680 FLOORBEAMAND RBL 44. REPLACED FITTING IAW DC9 SRM 51-30-2.

Part: PAN — CRACKED (PAX DOOR) · airframe 40,986 hrs · 45,575 cycles

DURING C-CHECK, FOUND MAIN ENTRY DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 51-30-2.

Part: LONGERON — CRACKED (BS 980)

DURING C-CHECK, FOUND LONGERON 17L CRACKED AT STATION 980. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LONGERON — CRACKED (BS 965)

DURING C-CHECK, FOUND LONGERON 17R CRACKED AT AFT SIDE OF PYLON BULKHEAD STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02.

Part: LINK — CRACKED (LT SPOILER)

DURING C-CHECK, FOUND THE LEFT INBOARD SPOILER DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 SMM 27-61-1 AND MM 27-61-0.

Part: LINK — CRACKED (LT SPOILER)

DURING C-CHECK, FOUND THE LEFT OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 SMM 27-61-1 AND MM 27-61-0.

Part: FITTING — CRACKED (BS 775)

DURING C-CHECK, FOUND THE FRAME FITTING AT STATION 775 AT LONGERON 24L CRACKED ON UPPER FLANGE. REPLACED FITTING IAW DC9 SRM 53-30-5, 51-30-2, 51-30-8 AND 51-30-1.

Part: FITTING — CRACKED (BS 945)

DURING C-CHECK, FOUND THE FRAME FITTING AT STATION 945 AND LONGERON 24L CRACKED ON INBOARD END OF LOWER FLANGE. REPLACED FRAME FITTING IAW DC9 SRM 51-30-5.

Part: WEB — CRACKED (BS 775-794)

DURING C-CHECK, FOUND CUSP WEB CRACKED IN 2 PLACES BETWEEN STATIONS 775 TO 794 LEFT SIDE, BL 20. REPAIRED WEB IAW DC9 SRM 53-01.

Part: WEB — CRACKED (BS 965)

DURING C-CHECK, FOUND CUSP WEB CRACKED OUTBOARD OF LBL 54 JUST FORWARD OF STATION 965. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: LONGERON — CORRODED (BS 756-840)

DURING C-CHECK, FOUND LONGERON 30 CORRODED BETWEEN FRAMES AT STATIONS 775 AND 794 AND AT STATION 756. REPLACED LONGERON BETWEEN STATIONS 756 AND 840 IAW DC9 SRM 51-30-5 AND 51-30-1.

Part: DOUBLER — CRACKED (PAX DOOR)

DURING C-CHECK, FOUND THE LEFT ENTRY DOOR EXTERNAL DOUBLER CRACKED AROUND THE HANDLE. REPLACED DOUBLER IAW DC9 SRM 51-30-2 AND DACO DWG 5910081.

Part: PRESSURE WEB — CORRODED (RT MLG WW)

DURING C-CHECK, FOUND THE CEILING PRESSURE PANEL STATION 737 EXFOLIATED ABOVE LONGERON 20. REPAIRED PRESSURE PANEL IAW ABX REA NR D 953-24434-MR.

Part: FRAME — CRACKED (BS 794)

DURING C-CHECK, FOUND THE FRAME AT STATION 794 CRACKED AT LONGERON 24L ON UPPER FLANGE. REPLACED FRAME FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (BS 965)

DURING C-CHECK, FOUND CUSP WEB CRACKED JUST FORWARD OF STATION 965, OUTBOARD OF RBL 54. REPAIRED CUSP WEB IAW DC9 SRM 53-01.

Part: PRESSURE WEB — CRACKED (NLG WW)

DURING C-CHECK, FOUND NOSE LANDING GEAR WHEEL WELL PRESSURE PANEL CRACKED AT STATION 83, RIGHT SIDE. REPAIRED PANEL IAW DC9 S/B 58-187.

Part: WEB — CORRODED (BS 755)

DURING C-CHECK, FOUND CUSP WEB CORRODED BETWEEN RBL 44 AND 55 AT STATION 755. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.

Part: FITTING — CRACKED (BS 362-370)

DURING C-CHECK, FOUND THE FITTING BETWEEN STATIONS 370 AND 362 AT LONGERON 30 CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.

Part: BUTE DOOR — DELAMINATED (WS 240)

WHILE COMPLYING WITH A C INSPECTON, FOUND THE LEFT WING BUTE DOOR NR 1502A DELAMINATED. REPLACED LEFT WING BUTE DOOR NR 1502A IAW DC-9 MAINTENANCE MANUAL CHAPTER 57-20-3.

Part: TRACK — WORN (BS 120)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE CAPTAINS FOWARD SEAT TRACK WORN. REPLACED CAPTAINS FOWARD SEAT TRACKS IAW DC-9 SRM CHAPTER 51-30-1 AND MAINTENANCE MANUAL CHAPTER 25-13-1.

Part: FAN CASE — CRACKED (NR 1 ENGINE)

WHILE COMPLYING WITH A C-INSPECTION, FOUND THE NR 1 ENGINE FORWARD FAN CASE MISSING MATERIAL AT THE 3, 5 AND 6 O'CLOCK POSITIONS. REPLACED THE NR 1 ENGINE FAN CASE IAW ABX JOB CARD BS 846A AND BS 8235 AND THE DC-9 MAINTENANCE MANUAL CHAPTERS 71-10-01 AND 71-10-02.

Part: PAN — DAMAGED (BS 200)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE FORWARD SERVICE DOOR JAMB DAMAGED AT BAYONET ROLLERS. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05 FIGURE 42.

Part: FAIRING — DELAMINATED (VERTICAL STAB)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE LEFT UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING DELAMINATED. REPLACED LEFT HAND UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING IAW ABD JOB CARD NR 40232.

Part: PAN — CORRODED (BS 370- 427)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR JAMB CORRODED AND BULGED BETWEEN FS 370 AND 427. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05 FIG 44 SHEET 2.

Part: SKIN — DAMAGED (BS 160)

WHILE COMPLYING WITH A C INSPECTION, FOUND THAT AIRCRAFT HAS AN INTERIM REPAIR INSTALLED AT FS 160, BELOW MAIN ENTRY THAT REQUIRES CLASS I REPAIR INSTALLED PROIR TO 12-17-96. REPAIRED IAW ABX REA D953-17390-MR.

Part: PANEL — DELAMINATED (WS 383-445)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE RIGHT WING TRAILING EDGE PANEL JUST OUTBOARD OF THE SPOILER DELAMINATED. REPLACED BONDED PANEL IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-2.

Part: LONGERON — CRACKED (BS 446)

WHILE COMPLYING WITH A C INSPECTION, FOUND LONGERON 4 LEFT CRACKED AT FS 446. REPAIRED LONGERON 4 LEFT IAW ABX REA D953-17397-MR.

Part: SCREW — RUSTED (VERTICAL STAB)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE VERTICAL STABILIZER CENTER ATTACH FITTINGS HAVE HEAVY RUST ON EIGHT EACH FASTENERS, AT FUSELAGE FRAME AT STATION 1104. REPLACED RUSTED FASTENERS IAW DC-9 SRM CHAPTER 51-30-1.

Part: RIB — CRACKED (VERTICAL STAB)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE ANGLED RIB IN THE VERTICAL STABILIZER REMOVEABLE LEADING EDGE SECTION CRACKED IN TWO PLACES. REPAIRED CRACKED RIB IAW SUP SRM DRAWING K05159.

Part: BUTE DOOR — DELAMINATED (WS 137)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE RIGHT WING BUTE DOOR NR 1601A DELAMINATED . REPLACED RIGHT WING BUTE DOOR NR 1601 IAW DC-9 MAINTENANCE MANUAL CHAPTER 57-20-3.

Part: TRACK — CORRODED (BS 897-965)

WHILE COMPLYING WITH A C INSPECTION, FOUND THE LEFT CARGO TIE DOWN TRACK IN THE AFT LOWER CARGO COMPARTMENT HAS EXFOLIATED CORROSION FROM FS 897 TO FS 965. REPLACED LEFT TRACK SECTION IAW DC-9 SRM CHAPTER 51-30-1.

Part: FAIRING — DELAMINATED (VERTICAL STAB)

WHILE COMPLYING WITH A C INSPECTON, FOUND THE RIGHT UPPER HORIZONTAL TO VERTICAL STABLIZER FAIRING DELAMINATED. REPLACED THE RIGHT UPPER HORIZONTAL TO VERTICAL STABLIZER FAIRING IAW ABX JOB CARD NR 40232.

Part: DOOR — CRACKED (CARGO COMPT)

WHILE COMPLYING WITH C INSPECTION, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR PAN CRACKED AT THE UPPER FORWARD STOP. REPLACED FORWARD LOWER CARGO COMPARTMENT DOOR IAW ABX JOB CARD C-3088.

Part: DOOR — CRACKED (CARGO COMPT)

WHILE COMPLYING WITH C INSPECTION, FOUND A CRACKED FITTING INSIDE THE FORWARD LOWER CARGO DOOR NEAR FORWARD HINGE. REMOVED AND REPLACED FORWARD BAG BIN DOOR IAW ABX JOB CARD C-3088.

Part: DOOR — CRACKED (CARGO COMPT)

WHILE COMPLYING WITH C INSPECTION, FOUND THE FORWARD LOWER CARGO DOOR INNER SKIN CRACKED AND BENT AT FORWARD HINGE. REMOVED AND REPLACED FORWARD BAG BIN DOOR IAW ABX JOB CARD C-3088.

Part: ENGINE — BIRD STRIKE (LEFT)

BIRD STRIKE LEFT ENGINE. REMOVED THE DAMAGED AREA TO THE LEFT ENGINE NR 1 BLADE, BORESCOPED THE LEFT ENGINE AND GROUND RAN TO TAKEOFF EPR, OPS CHECKED GOOD.

Part: SKIN — CORRODED (CARGO DOOR)

FOUND FWD LWR CARGO DOOR PAN CORRODED AND CRACKED, INTERCOSTAL CRACKED, AND DOOR SKIN CRACKED. REPAIRED SKIN (P/N 5910141-27) IAW REA D952-17254. REPLACED INTERCOSTAL (P/N 9957664-2) IAW DC9 DWG - 5910141. REPLACED PAN (P/N 5910141-7, 5910141-9) IAW DC9 DWG - 5910141.

Part: DNLOCK SWITCH — INTERMITTENT (RT MLG)

RIGHT MAIN GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT CAME ON. RECYCLED GEAR AND ALL INDICATIONS WERE NORMAL. REPLACED MAIN GEAR DOWNLOCK SWITCH IAW DC-9 SUPP. M.M. OPS CHECKED GOOD.

Part: FRAME — DAMAGED (BS 897)

DURING C-CHECK INSPECTION, AN ELONGATED BARREL NUT HOLE WAS DISCOVERED BETWEEN LONGERONS 27R AND 28R AT STA 897. REPAIRED IAW ABX REA D953-12783-MR.

Part: DOUBLER — DAMAGED (PAX DOOR AREA)

DURING C-CHECK INSPECTION AN EXISTING REPAIR WAS FOUND DAMAGED ON THE FORWARD UPPER CORNER OF THE FORWARD ENTRY DOOR. REPAIRED IAW ABX REA D953-12658-MR.

Part: VANE — DENTED (LT WING)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, THE LEFT WING UPPER MOVEABLE VANE WAS FOUND DENTED. REPLACED VANE IAW DC-9 MM 27-51-2.

Part: FLOORBEAM — CORRODED (BS 294)

DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FLOORBEAM AT STA 294, LBL 1. REPAIRED IAW ABX REA D953-12742-MR.

Part: FITTING — CRACKED (BS 965)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A FITTING CRACKED ON THE AFT SIDE OF A FLOORBEAM AT STA 965, RBL 49. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 996)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 996, LONGERON 18R. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CRACKED (BS 996)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 996, LONGERON 18L. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-2 AND 51-30-5.

Part: SHEAR TIE — CRACKED (FS 950)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 92-22-08, FOUND A CRACKED SHEAR TIE AT STA 950, LONGERON 15R. REPLACED SHEAR TIE IAW DC-9SRM 51-30-2 AND 51-30-5.

Part: BUSHING — WORN (LT MLG DOOR)

DURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 91-22-07, ASB 32-244, FOUND THE LEFT MAIN OUTBOARD LANDING GEAR DOOR HINGE WORN. HINGE BUSHINGS REPLACED IAW DC-9 MM 32-12-1.

Part: SKIN — GOUGED (BS 440)

DURING C-CHECK INSPECTION, THE FUSELAGE SKIN AT STA 440 AND LONGERON 16L WAS FOUND GOUGED. REPAIRED IAW ABX REA D953-12668-MR.

Part: EEL BATTERY — DISCHARGED (CABIN)

COCKPIT EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERIES. OPS CHECKED GOOD IAW DC-9 M.M. 33-53-0.

Part: FRAME — GOUGED (AFT PRESS BLKHD)

DURING COMPLIANCE OF A.D. 79-24-01; S.B. 53-127, FOUND GOUGE AT 10 O'CLOCK POSITION ON PLUG DOOR STOP. BLENDED OUT GOUGE AT 10 O'CLOCK POSITION IAW DC-9 SRM 51-01.